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AN APPROXIMATE METHOD FOR CALCULATING THE LAMINAR BOUNDARY LAYER ON AN INFINITE SWEPT WING WITH ARBITRARY VELOCITY AND SUCTION DISTRIBUTIONS.

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BookPublisher: Her Majesty'S Stationery Office, London 1957Description: 19.DDC classification: ARC | C.P. 516

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	ARC C.P. 516 (Browse shelf)	Not for loan		TR10943

Total holds: 0

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Previous	ARC C.P. 513 A PRELIMINARY NOTE ON A MODIFIED TYPE OF AIR JET FOR BOUNDARY-LAYER CONTROL.	ARC C.P. 514 WIND TUNNEL MEASUREMENTS OF LIFE, DRAG AND PITCHING MOMENT OF TWO HIGHLY SWEPT (;E =87DEGREE AND 81DEGREE) DELTA WING-BODY COMBINATION MODELS WITH SMALL TIP FINS AT M=2.47	ARC C.P. 515 STATIC TESTS ON A CONICAL CENTREBODY SUPERSONIC AIR INTAKE WITH AN AUXILIARY AIR INLET SLOT.	ARC C.P. 516 AN APPROXIMATE METHOD FOR CALCULATING THE LAMINAR BOUNDARY LAYER ON AN INFINITE SWEPT WING WITH ARBITRARY VELOCITY AND SUCTION DISTRIBUTIONS.	ARC C.P. 517 WIND TUNNEL EXPERIMENTS ON A MODEL OF A TANDEM ROTOR HELICOPTER.	ARC C.P. 518 SOME TESTS ON AVON-CANBERRA INSTALLATION TO MEASURE THRUST IN FLIGHT.	ARC C.P. 519 WIND TUNNEL MEASUREMENTS OF THE LIFE-DEPENDENT DRAG OF THIN CONICALLY CAMBERED SLENDER DELTA WINGS AT MACH NUMBERS 1.4 AND 1.8	Next

Bound With Arc C.P.511-515, 517-20

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